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To: Blennos
That it was. Yet, to the credit of the YF-22, it had two weapons bays and greater stealthy internal weapons carriage space than the YF-23, which ruthlessly applied the drag-reducing area rule design principle. This resulted in a gracile and sinuous shape for the YF-23 and gave it exceptional speed and range.

Although it would have been expensive, the US would have been better off to have completed development of both the F-22 and F-23 to keep the contractors putting out their best efforts on price, quality, and schedule. Moreover, even with the F-22 as the preferred type, a relatively small production run of the F-23 would provide US commanders with the relative advantages of both.

In combat, for example, a five to one ratio of F-22s and F-23s would give the US the ability to use the speed of F-23s for a rapid initial contact and missile volley, with the F-22s then arriving in order to use its maneuverability in a dogfight or its larger internal weapons capacity for bombing missions. Having both types available would also complicate mission planning by our adversaries.

Some observers suspect that US built a small number of F-23s for strategic reconnaissance purposes. Or at least that may be why key performance data remains secret for an aircraft that -- officially -- never went into production.

8 posted on 11/13/2015 6:40:31 AM PST by Rockingham
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To: Rockingham
"hich ruthlessly applied the drag-reducing area rule design principle. This resulted in a gracile and sinuous shape for the YF-23 and gave it exceptional speed and range."

Ah, a fan of Mr. Witcomb I see, ;-) are you aware of the "poor man's area rule" via John Thorp? Google: adverse pressure gradient matching ar-5 to find the link...

13 posted on 11/13/2015 8:02:29 AM PST by taildragger (Not my Monkey, not my Circus...)
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